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Preliminary performance of the brayton 4.25 inch radial compressor operating in a helium xenon gas mixture
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Asadourian, A. S. Hecker, T. P. Kruchowy, R. |
| Copyright Year | 1971 |
| Description | Compressor performance was mapped during the Brayton cycle power system testing. The range of testing included three shaft speeds: the design speed of 36,000 rpm, 10 percent overspeed (39,600 rpm), and 10 percent underspeed (32,400 rpm). A range of compressor inlet temperatures from 60 F to 120 F and discharge pressures from 20 to 45 psia were included. The effects of turbine inlet temperatures (from 1200 F to 1600 F) on the compressor were also studied. The data presented include plots of weight flow, compressor pressure ratio, efficiency, and temperature-rise ratio. |
| File Size | 2135045 |
| Page Count | 36 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720008340 |
| Archival Resource Key | ark:/13960/t7wm61s00 |
| Language | English |
| Publisher Date | 1971-12-01 |
| Access Restriction | Open |
| Subject Keyword | Auxiliary Systems Turbocompressors Brayton Cycle Radial Distribution Helium Xenon Gas Mixtures Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
